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DA40-180
D I A M O N D S T A R
Q U I C K R E F E R E N C E H A N D B O O K
R e v i s i o n 1 . 3
E F F : 0 8 - 1 3 - 2 0 1 0
D o c u m e n t L e v e l : 3
AIRLINE TRAINING CENTER, INC.
I N T E N T I O N A L L Y L E F T B L A N K
REV 1.3 —
QRH DA40-180
Document Level: 3
PITCH-POWER TABLE ........................................................ 1
MANEUVERS ...................................................................... 2
NORMAL PROCEDURES ...................................................... 3
EMERGENCY PROCEDURES ................................................. 4
PATTERNS ........................................................................ 5
LIMITATIONS .................................................................... 6
WEIGHT AND BALANCE ...................................................... 7
PERFORMANCE.................................................................. 8
TABLE OF CONTENT AIRLINE TRAINING CENTER, INC.
WARNING!
This QRH is to be used for training purposes only within SATC/SFA. In case there is a
discrepancy between the AFM/POH or this QRH, the AFM/POH will overrule the
procedures, limitations, performance or systems described in this POH.
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0.1
I N T E N T I O N A L L Y L E F T B L A N K
PITCH
POWER
TABLE
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I N T E N T I O N A L L Y L E F T B L A N K
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PITCH POWER AIRLINE TRAINING CENTER, INC. 1.1
TAKEOFF
VR 60 KIAS FLAPS T.O. ROTATION FULL / MAX +9
CLIMB
70 KIAS CLEAN > 300 AGL FULL / 2400 +10
75 KIAS CLEAN > 1.000 AGL FULL / 2400 +8
LEVEL
65 KIAS CLEAN SLOW FLIGHT 17 / MAX +7
100 KIAS CLEAN 19 / 2400 +2
105 KIAS CLEAN 20 / 2400 +1
110 KIAS CLEAN 21 / 2400 0
120 KIAS CLEAN 24 / 2400 -1
DESCENT 500FPM
120 KIAS CLEAN 17 / 2400 -2
110 KIAS CLEAN 15 / 2400 -2
90 KIAS FLAPS T/O INSTR APCH 14 / MAX -5
SPEED CONF ALT/PHASE MAP / RPM BODY
ATTITUDE (°)
NORMAL TRAFFIC PATTERN
100 KIAS CLEAN DOWNWIND 19 / 2400 +2
90 KIAS FLAPS T/O DOWNWIND 19 / 2400 - 1
80 KIAS FLAPS T/O BASELEG 15 / 2400 -3
70 KIAS FLAPS LDG FINAL 19 / MAX AIMING POINT
QRH DA40-180
REV 1.3 —
Document Level: 3
SPEED CONF ALT/PHASE MAP / RPM BODY
ATTITUDE (°)
AIRLINE TRAINING CENTER, INC. PITCH POWER
1.2
FLAPLESS PATTERN
100 KIAS CLEAN DOWNWIND 18 / 2400 +2
90 KIAS CLEAN DOWNWIND 18 / 2400 +2
85 KIAS CLEAN BASELEG 13 / 2400 -1
75 KIAS CLEAN FINAL 14 / MAX AIMING POINT
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MANEUVERS
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I N T E N T I O N A L L Y L E F T B L A N K
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MANEUVERS AIRLINE TRAINING CENTER, INC. 2.1
SPEEDS
NORMAL CLIMB 70 KIAS < 1.000 FT AGL
NORMAL CLIMB 75 KIAS > 1.000 FT AGL
BEST RATE OF CLIMB
(FLAPS T/O) 60 KIAS @ 2,205 LBS 66 KIAS @ 2,535 LBS
TO EXPEDITE CLIMB 70 KIAS FULL POWER / MAX RPM
NORMAL CRUISE 110 KIAS < 5 .000 FT MSL
NORMAL CRUISE 120 KTAS > 5.000 FT MSL
VFR MANEUVERS 100 KIAS
MAX SPEED
LIGHT TURBULENCE 129 KIAS (Vno)
MAX SPEED
ROUGH AIR
108 KIAS > 2,161 LBS
(Va)
94 KIAS < 2,161 LBS
(Va)
TO EXPEDITE DESCENT AS REQUIRED 1.000 FPM
QRH DA40-180
REV 1.3 —
Document Level: 3
SPEEDS
IFR HOLDING 100 KIAS CLEAN
IFR COURSE REVERSAL 100 KIAS CLEAN
IFR APPROACH SPEED 90 KIAS FLAPS T/O
AIRLINE TRAINING CENTER, INC. MANEUVERS
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MANEUVERS AIRLINE TRAINING CENTER, INC. 2.3
SLOW FLIGHT
DECELERATION
SPEED ............................................................................... 100 KIAS
POWER .......................................... REDUCE TO 12‖ MAP / MAX RPM
ALTITUDE ........................................................................ MAINTAIN
BA ................................................... GRADUALLY INCREASE TO + 7°
SPEED ................................................................................ 65 KIAS
POWER ............................................................................... 17‖ MAP
Trim
ACCELERATION
POWER ....................................................... FULL POWER / MAX RPM
ALTITUDE ........................................................................ MAINTAIN
BA .................................................... GRADUALLY DECREASE TO +2°
SPEED ............................................................................... 100 KIAS
POWER .................................................................... 19‖ / 2400 RPM
Trim
STEEP TURNS
SPEED ............................................................................... 100 KIAS
BANK ANGLE ........................................ NORMAL ROLL RATE TO 45°
BA ...................................................................... INCREASE TO 2.5°
POWER ........................................................................ INCREASE 2‖
RUDDER .................................... AS REQUIRED TO CENTER SIDE SLIP
Do not trim
HEADING ........................................... 15 ° BEFORE INITIAL HEADING
BANK ..................................................... NORMAL ROLL RATE TO 0°
BA ........................................................................ DECREASE TO +2°
POWER .................................................................... 19‖ / 2400 RPM
Control the roll to repeat exercise in opposite direction.
RUDDER .................................... AS REQUIRED TO CENTER SIDE SLIP
QRH DA40-180
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AIRLINE TRAINING CENTER, INC. MANEUVERS
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STALLS
STANDARD RECOVERY TECHNIQUE
VALID FOR ALL STALL EXERCISES
AS THE NOSE STARTS TO DROP
1—BODY ATTITUDE ........................ SLIGHTLY BELOW THE HORIZON
2—POWER ............................................................................... FULL
IF A WING SHOULD DROP
RUDDER ............................................... OPPOSITE TO PREVENT YAW
SPEED ................................................................... CHECK > 65 KIAS
AILERONS ................................................. USE TO LEVEL THE WINGS
WHEN FLYING SPEED HAS BEEN REGAINED
3—RECOVERY ......... SEE BELOW ACCORDING TO THE TYPE OF STALL
BEFORE (EACH) STALL EXERCISE—VITAL ACTIONS
H HEIGHT ........................................................ ABOVE 2,300 FT AGL
A AREA .......................................... OUT OF CONTROLLED AIRSPACE
................................................... NOT ABOVE TOWNS OR AIRFIELDS
C COCKPIT ............................................ NO LARGE LOOSE ARTICLES
..................................................... SEATS AND SEAT BELTS SECURES
...................................................... ENGINE INSTRUMENTS IN LIMITS
L LOOKOUT ................................. 180° OR 2x90° CLEARING TURN(S)
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MANEUVERS AIRLINE TRAINING CENTER, INC. 2.5
STALL (CLEAN)
0° BANK—52 KIAS
IDLE—FORWARD CG—MAX WEIGHT
ENTRY
SPEED ............................................................................... 100 KIAS
POWER ................................................. REDUCE TO IDLE / MAX RPM
ALTITUDE ........................................................................ MAINTAIN
TRIM ................................................ DO NOT TRIM BELOW 65 KIAS
RECOVERY
POWER ..................................................................................... FULL
SPEED ........................................ ACCELERATING THROUGH 65 KIAS
BA ........................................................................... ROTATE TO +9°
SPEED .................................................................MAINTAIN 75 KIAS
ALTITUDE ............................................. CLIMB TO INITIAL ALTITUDE
HEADING ...................................... TURN BACK TO INITIAL HEADING
LEVEL OFF AT INITIAL ALTITUDE
BA .................................................... GRADUALLY DECREASE TO +2°
SPEED ............................................................................... 100 KIAS
POWER .................................................................... 19‖ / 2400 RPM
QRH DA40-180
REV 1.3 —
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AIRLINE TRAINING CENTER, INC. MANEUVERS
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TAKEOFF STALL (POWER—ON / CLEAN)
NO AFM DATA ON EXACT STALL SPEED AVAILABLE
EXPECT ACTUAL STALL SPEED TO BE BELOW 50 KIAS (0° BANK)
ENTRY
SPEED ................................................................................ 100 KIAS
POWER ................................................................... 19‖ / 2400 RPM
POWER .................................................................... 12‖ / MAX RPM
WHEN PASSING THROUGH 70 KIAS:
BA ............................................................................ RAISE TO +20°
POWER ........... FULL POWER or 17‖ / MAX RPM (UP TO INSTRUCTOR)
TRIM ................................................ DO NOT TRIM BELOW 65 KIAS
RECOVERY
POWER .................................................................................... FULL
SPEED ......................................... ACCELERATING THROUGH 65 KIAS
BA .......................................................................... ROTATE TO +9°
SPEED ................................................................. MAINTAIN 75 KIAS
ALTITUDE .............................................. BACK TO INITIAL ALTITUDE
HEADING ...................................... TURN BACK TO INITIAL HEADING
LEVEL OFF AT INITIAL ALTITUDE
SPEED ................................................................................ 100 KIAS
POWER ................................................................... 19‖ / 2400 RPM
Trim
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MANEUVERS AIRLINE TRAINING CENTER, INC. 2.7
LANDING STALL (POWER—OFF / FLAPS LDG)
0° BANK—49 KIAS
IDLE—FORWARD CG—MAX WEIGHT
ENTRY
SPEED ............................................................................... 100 KIAS
POWER .................................................................... 19‖ / 2400 RPM
USE TRAFFIC PATTERN SEQUENCE TO ARRIVE AT FINAL
CONFIGURATION (LDG FLAPS—75KIAS)
POWER .................................................................... 14‖ / 2400 RPM
SPEED ................................................................................. 75 KIAS
FLIGHT PATH ............................. ESTABLISH A STABILIZED DESCENT
TRIM .................................................................. TRIM FOR 75 KIAS
POWER ..................................... IDLE & SIMULATE A FLARE TO LAND
RECOVERY
POWER ................................................................... FULL / MAX RPM
FLAPS ................................................................................ TAKEOFF
SPEED ................................................................................. 65 KIAS
BA ........................................................................... ROTATE TO +9°
ALTIMETER & VSI ..................................................... POSITIVE CLIMB
―POSITIVE CLIMB‖
SPEED .............................................................................. > 70 KIAS
FLAPS .......................................................................................... UP
SPEED .................................................................MAINTAIN 75 KIAS
ALTITUDE ............................................. CLIMB TO INITIAL ALTITUDE
HEADING ...................................... TURN BACK TO INITIAL HEADING
LEVEL OFF AT INITIAL ALTITUDE
BA .................................................... GRADUALLY DECREASE TO +2°
SPEED ............................................................................... 100 KIAS
POWER .................................................................... 19‖ / 2400 RPM
Trim
QRH DA40-180
REV 1.3 —
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AIRLINE TRAINING CENTER, INC. MANEUVERS
2.8
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SPIN RECOVERY
Spins are NOT allowed on the DA40 as per AFM/POH.
Aerobatics and flight maneuvers with high bank angle are usually
pilots voluntarily executed maneuvers.
A Spin on the contrary is usually a result of pilot error while maneu-
vering at low speeds.
Do remember that since the majority of fatal stall/spin accidents oc-
cur at low altitudes, from which recovery is unlikely, prevention is
essential.
APPROVED MANEUVERS
a) Normal Category:
CAUTION
Aerobatics, spinning, and flight maneuvers with more than
60° of bank are not permitted in the Normal Category.
b) Utility Category:
CAUTION
Aerobatics, spinning, and flight maneuvers with more than
90° of bank are not permitted in the Utility Category.
WARNING
When exceeding 60° of bank the wearing of a parachute is man-
datory.
REV 1.3 —
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Document Level: 3
FLAPLESS PATTERN
SEE ALSO CHAPTER ‗PATTERNS‘
SPEEDS
ALL TARGET PATTERN SPEEDS ....................................ADD 5 KNOTS
KEYPOINTS
- BODY ATTITUDES ............ WILL BE HIGHER THAN NORMAL (TRIM!!)
- DOWNWIND ..................................... EXTEND SLIGHTLY (1/4 MILE)
- SLOPE ........................................ FLY A NORMAL 3° SLOPE TO RWY
- FLARE............................... APPLY REDUCED FLARE—DON‘T FLOAT
- GO—AROUND ............................. ― GO-AROUND, FLAPS UP‖
GO—AROUND
―GO—AROUND, FLAPS!‖
POWER ..................................................................................... FULL
BA ........................................................................... ROTATE TO +9°
FLAPS ............................. TAKEOFF (EXCEPT IF FLAPLESS APPROACH)
ALTIMETER & VSI ..................................................... POSITIVE CLIMB
―POSITIVE CLIMB‖
SPEED .......................................................... CHECK ABOVE 70 KIAS
FLAPS .......................................................................................... UP
SPEED .................................................................MAINTAIN 75 KIAS
―AFTER TAKEOFF CHECKLIST‖
MANEUVERS AIRLINE TRAINING CENTER, INC. 2.9
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AIRLINE TRAINING CENTER, INC. MANEUVERS
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TOUCH & GO
DURING THE TOUCH AND GO ROLL:
FLAPS ....................................................... UP (BY THE INSTRUCTOR)
VERIFY WITH INSTRUCTOR PRIOR TO RETRACTING FLAPS
―TAKEOFF, YOU HAVE CONTROL‖
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MANEUVERS AIRLINE TRAINING CENTER, INC. 2.11
SHORT FIELD TAKEOFF
ALL TAKEOFFS ARE PERFORMED WITH FLAPS T/O
TAKEOFF
BRAKES .................................................................................. HOLD
POWER ..................................................................................... FULL
ENGINE INSTRUMENTS ........................................................... CHECK
BRAKES .............................................................................. RELEASE
SPEED ............................ CHECK INCREASING—ROTATE AT 60 KIAS
CLIMB
ALTIMETER & VSI ..................................................... POSITIVE CLIMB
―POSITIVE CLIMB‖
BA ............................................................................................ +10°
SPEED .................................................................MAINTAIN 66 KIAS
WHEN CLEAR OF OBSTACLES
SPEED ......................................................................... ACCELERATE
SPEED .............................................................................. > 70 KIAS
FLAPS .......................................................................................... UP
SPEED ............. ACCELERATE TO NORMAL CLIMB 75 KIAS/2400 RPM
―AFTER TAKEOFF CHECKLIST‖
SHORT FIELD LANDING
FINAL TURN COMPLETED
FLAPS ........................................................................................ LDG
SPEED ................................................................................. 70 KIAS
WHEN CLEAR OF OBSTACLES
BA .................................................................. AIM FOR THRESHOLD
POWER .............................................................ADJUST FOR 70 KIAS
TOUCHDOWN
BRAKES ............................................................ APPLY (GRADUALLY)
I N T E N T I O N A L L Y L E F T B L A N K
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NORMAL
PROC
I N T E N T I O N A L L Y L E F T B L A N K
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.1
INTRODUCTION
BEFORE EVERY FLIGHT DEPARTING FROM HOME BASE
1/ COMPANY INFORMATION ............................. CHECK ON WEBSITE
(BULLETINS—WARNINGS—LATEST DOCUMENTS)
2/ WEATHER / NOTAMS / TFR’S ............................................ CHECK
USE WEBSITE OR 1-800-WX-BRIEF BY PHONE
3/ ATIS .............................. OBTAIN THROUGH RADIO AT DISPATCH
4/ FLIGHT RELEASE FORM .................................. PRINT & COMPLETE
5/ AIRCRAFT TECHNICAL LOG ...............................CHECK SQUAWKS
6/ REQUIRED EQUIPMENT ...................................................... CHECK
7/ AIRCRAFT POUCH ................................. OBTAIN FROM DISPATCH
CHECK CONTENT (KEYS—FUEL CARD—LOGBOOK)
8/ I-M-S-A-F-E CHECKLIST .................................................. CHECK
9/ MISSION BRIEFING ............................................................ CHECK
NOTES
A black triangle (sideways) printed in front of a checklist or flow item, indi-
cates optional equipment and must be read as ―if installed…‖.
Indicates a call out (to be performed out loud).
QRH DA40-180
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.2
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PROCEDURES FOR CHECKLISTS AND FLOWS
Student in the left seat—Instructor in the right seat. Student will perform
all flying duties, and scans and actions (flows), and all checklists, except
the ones shown in the table as ‗PM‘ - ‗Pilot Monitoring‘. The reader will
announce the start of any checklist by calling out its title, and will read
all items out loud (with sufficient pause between the items for verifica-
tion and/or answer), and will announce the checklist completed by an-
nouncing its title + …‖COMPLETED‖.
‗PM‘ - ‗Pilot Monitoring‘ will be the instructor. For single-pilot opera-
tions, all items listed in the table below under ‗PM‘ will have to be per-
formed by the ‗PF‘. All students must be proficient in operating the DA-
40 in a single-pilot environment.
FLOW AND CHECKLIST HANDLING
Phase of Flight
Flow Checklist
Performed by Loud or
Silent Performed by
Loud or
Silent
Before Start PF Loud PM Loud
After Start PF Loud PM Loud
Before Takeoff PF Loud PM Loud
Line Up PM Silent N/A N/A
After Takeoff PF Silent PF (by heart) Loud
Descent /
Approach PF Silent PF (by heart) Loud
Landing PF Silent PF (by heart) Loud
After Landing PM Silent PM Silent
Shutdown PF Loud PF Loud
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.3
Through flight = same day, same airplane, same crew.
Through flight walk around = fuel, oil and tires only.
All cockpit flows must be read out loud.
APPROACHING THE AIRCRAFT
NEARBY OBSTACLES .................................................................. CHECK
FLAP POSITION ........................................................................... NOTE
The flap position should be noted before boarding the airplane.
SURFACES ................................................................................. CLEAR
Check that all movable surfaces are clear and can be moved without
hitting obstacles.
ANTENNAS ............................................................................... CHECK
Check presence and condition of following antennas: COM, NAV,
transponder, ELT.
PRELIMINARY INSPECTION
Be careful not to use the top of the instrument panel as a support
when entering or exiting the aircraft. Use the dedicated handle behind
the glareshield for support.
FRONT AND REAR CANOPY ...................................................... CHECK
Verify that the canopy is clean and undamaged. Check for cracks
and major scratches. Check locking mechanism. To avoid scratch-
ing the paint or damaging the wing, do not sit or put any equip-
ment on the wing. Do not use the top of the instrument panel as a
shelf for equipment at any time. Make sure not to touch the canopy
with hands, equipment or charts.
FIRE EXTINGUISHER ................................. CHECK SECURE/ CONDITION
QRH DA40-180
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CONTROL LOCKS ................................................................... REMOVE
IGNITION KEY .................................................................... CHECK OFF
HOBBS METER .......................................................................... CHECK
UPPER SWITCH PANEL ............................................. ALL SWITCHES OFF
LOWER SWITCH PANEL ........................................... ALL SWITCHES OFF
Check pitot heat off, fuel pump off, start key pulled out, electric
master off and avionics master off.
PARKING BRAKE SET ...................................................................... SET
To set the parking brake: set parking brake on, then pump the
brake pedals to build up pressure in the brake cylinder.
ELECTRIC MASTER SWITCH ............................................................. ON
Turn on both the BATT & ALT side. Allow the G1000 to initialize.
Check database validity on MFD. Press ‗ENT twice on the MFD
(lower right softkey).
FLAPS ........................................................................................... LDG
Set the FLAPS to T/O, monitor flap extension and indication. Then
set FLAPS to LDG, monitor flap extension and indication. Leave
FLAPS in LDG position for walkaround.
FUEL GAUGES .......................................................... CHECK QUANTITY
ELECTRIC MASTER SWITCH ............................................................ OFF
TRIM ..................................................................................... NEUTRAL
Check full control travel (both ways) of elevator trim, then, in
preparation for the walk around, set in neutral position.
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.5
SUNSCREENS, PITOT COVER, TIE DOWN, CHOCKS ................ REMOVED
Put sunscreens (if available) in their dedicated bag. Put pitot cover
in the flight gear bag. If the aircraft‘s own tie-down ropes and
wheel clocks were used, put in the flight gear bag.
TOW BAR ............................................................... PROPERLY STOWED
REQUIRED EQUIPMENT ....................................................... ON BOARD
The following equipment must be on board:
Aircraft pouch containing: aircraft flight time log book, emergency
sick sacs, fuel card & keys.
Bag containing sunscreens for the windows (if available) .
Flight gear bag containing: fuel tester, flip-up training glasses,
flash light, wheel chocks, pitot cover, 3 tie-down ropes, first aid kit.
Fire extinguisher.
Rescue hammer.
EASA/FAA approved airplane flight manual (POH).
JAA/FAA required documents: certificate of airworthiness, airplane
registration.
Alternate fuel measuring device
G1000 User manual
QRH DA40-180
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WALK AROUND
Walkaround is counterclockwise around the aircraft.
LEFT MAIN LANDING GEAR
LANDING GEAR STRUT .......................................... VISUAL INSPECTION
Check visually and verify no damage or cracks.
WEAR, TREAD DEPTH OF TIRE ................................ VISUAL INSPECTION
Tires should be taken out of service when they have one or more
flat spots. Generally, a single flat spot or skid burn does not expose
the carcass body and the tire may remain in service, unless severe
unbalance is reported by the crew. Small cuts are acceptable, if they
do not protrude into the tire carcass. Cuts in the side wall are not
acceptable. Shallow chevron-shaped cuts across the tread of a tire
pose no problem; they are caused by landing on a grooved concrete
runway. As long as the tread does not wear down into the body
plies of the carcass, the basic strength of the tire is not affected. To
provide traction during wet runway operation, operators should
replace their tires when the tread reaches 1 / 32 inch = 0.79 mm.
WHEEL & BRAKES ................................................... VISUAL INSPECTION
When checking the brakes: verify that there is even wear on the
disc, no scratches, no grease, and no leaks near the brake line.
SLIP MARKS ........................................................... VISUAL INSPECTION
CHOCKS ................................................................................. REMOVE
LEFT WING
ENTIRE WING SURFACE .......................................... VISUAL INSPECTION
STEP ...................................................................... VISUAL INSPECTION
AIR INTAKE ON LOWER SURFACE ........................... VISUAL INSPECTION
OPENINGS ON LOWER SURFACE ............................. VISUAL INSPECTION
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.7
Check for foreign objects and for traces of fuel (if tank is full, fuel
may spill over through the tank vent).
TANK DRAIN ........................................... DRAIN / VISUAL INSPECTION
Check for water and sediment (drain until no water or sediment
comes out.
STALL WARNING DEVICE ....................................... VISUAL INSPECTION
TANK FILLER .............................. VISUAL INSPECTION / CHECK CLOSED
Fuel quantity must agree with indicator.
2 STALL STRIPS ON WING ...................................... VISUAL INSPECTION
PITOT STATIC PROBE ................................................................ CHECK
Check pitot probe is clean, orifices clear, cover removed and no
deformation.
TIE-DOWN .................................................................. CHECK / CLEAR
LANDING / TAXI LIGHT ......................................... VISUAL INSPECTION
WING TIP .............................................................. VISUAL INSPECTION
POSITION LIGHT, STROBE LIGHT (ACL) .................. VISUAL INSPECTION
AILERON AND LINKAGE ......................................... VISUAL INSPECTION
AILERON HINGES AND SAFETY PIN......................... VISUAL INSPECTION
FOREIGN OBJECTS IN AILERON PADDLE ................. VISUAL INSPECTION
FLAP AND LINKAGE ............................................... VISUAL INSPECTION
FLAP HINGES AND SAFETY PIN............................... VISUAL INSPECTION
FUSELAGE, LEFT SIDE
CANOPY, LEFT SIDE ............................................... VISUAL INSPECTION
REAR CABIN DOOR & WINDOW .............................. VISUAL INSPECTION
FUSELAGE SKIN ..................................................... VISUAL INSPECTION
ANTENNAS ............................................................ VISUAL INSPECTION
EMPANNAGE
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STABILIZERS AND CONTROL SURFACES, ELEVATOR TIPS ......................
............................................................................. VISUAL INSPECTION
HINGES ................................................................. VISUAL INSPECTION
ELEVATOR TRIM TAB ............ VISUAL INSPECTION / CHECK SAFETYING
RUDDER TRIM TAB ................................................ VISUAL INSPECTION
TIE-DOWN .................................................................. CHECK / CLEAR
TAIL SKID AND LOWER FIN .................................... VISUAL INSPECTION
FUSELAGE, RIGHT SIDE
FUSELAGE SKIN...................................................... VISUAL INSPECTION
WINDOW ............................................................... VISUAL INSPECTION
CANOPY, RIGHT SIDE ............................................. VISUAL INSPECTION
RIGHT WING
FLAP AND LINKAGE .............................................. VISUAL INSPECTION
FLAP HINGES AND SAFETY PIN ............................... VISUAL INSPECTION
AILERON AND LINKAGE ......................................... VISUAL INSPECTION
AILERON HINGES AND SAFETY PIN ......................... VISUAL INSPECTION
FOREIGN OBJECTS IN AILERON PADDLE .................. VISUAL INSPECTION
WING TIP ............................................................... VISUAL INSPECTION
POSITION LIGHT, STROBE LIGHT (ACL) ................... VISUAL INSPECTION
TIE-DOWN .................................................................. CHECK / CLEAR
ENTIRE WING SURFACE .......................................... VISUAL INSPECTION
2 STALL STRIPS ON WING ...................................... VISUAL INSPECTION
TANK FILLER ............................. VISUAL INSPECTION / CHECK CLOSED
Fuel quantity must agree with indicator.
OPENINGS ON LOWER SURFACE ............................. VISUAL INSPECTION
Check for foreign objects and for traces of fuel (if tank is full, fuel
may spill over through the tank vent).
TANK DRAIN ........................................... DRAIN / VISUAL INSPECTION
Check for water and sediment (drain until no water or sediment
comes out.
STEP ...................................................................... VISUAL INSPECTION
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.9
LANDING GEAR STRUT .......................................... VISUAL INSPECTION
Check visually and verify no damage or cracks.
WEAR, TREAD DEPTH OF TIRE ............................... VISUAL INSPECTION
Tires should be taken out of service when they have one or more
flat spots. Generally, a single flat spot or skid burn does not expose
the carcass body and the tire may remain in service, unless severe
unbalance is reported by the crew. Small cuts are acceptable, if they
do not protrude into the tire carcass. Cuts in the side wall are not
acceptable. Shallow chevron-shaped cuts across the tread of a tire
pose no problem; they are caused by landing on a grooved concrete
runway. As long as the tread does not wear down into the body
plies of the carcass, the basic strength of the tire is not affected. To
provide traction during wet runway operation, operators should
replace their tires when the tread reaches 1 / 32 inch = 0.79 mm.
WHEEL & BRAKES .................................................. VISUAL INSPECTION
When checking the brakes: verify that there is even wear on the
disc, no scratches, no grease, and no leaks near the brake line.
SLIP MARKS ........................................................... VISUAL INSPECTION
CHOCKS ................................................................................ REMOVE
FUSELAGE, FRONT
ENGINE OIL LEVEL ..................................................................... CHECK
Check oil level through inspection hole in upper cowling. Normal oil
quantity is 5.5 quarts. Minimum is 4 quarts for VFR, and 6 quarts
for IFR. Do not refill when oil quantity is above 7.5 quarts.
COWLING .............................................................. VISUAL INSPECTION
3 AIR INTAKES .......................................................................... CLEAR
PROPELLER & SPINNER ........................................... VISUAL INSPECTION
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Check no detrimental nicks, cracks or dents in propeller blades,
and no traces of oil (leak in the CSU). Check blades no excessive
play in CSU. Maximum blade shake 3mm (1/8 inch), maximum
angular play of blade: 2°. Check spinner attachment screws.
NOSE LANDING GEAR STRUT ................................. VISUAL INSPECTION
Check visually and verify no damage or cracks.
WHEEL ................................................................... VISUAL INSPECTION
WEAR, TREAD DEPTH OF TIRE ................................ VISUAL INSPECTION
Tires should be taken out of service when they have one or
more flat spots. Generally, a single flat spot or skid burn does not
expose the carcass body and the tire may remain in service, unless
severe unbalance is reported by the crew. Small cuts are acceptable,
if they do not protrude into the tire carcass. Cuts in the side wall
are not acceptable. Shallow chevron-shaped cuts across the tread
of a tire pose no problem; they are caused by landing on a grooved
concrete runway. As long as the tread does not wear down into the
body plies of the carcass, the basic strength of the tire is not af-
fected. To provide traction during wet runway operation, operators
should replace their tires when the tread reaches 1 / 32 inch =
0.79 mm.
SLIP MARKS ........................................................... VISUAL INSPECTION
CHOCKS ................................................................................. REMOVE
EXHAUST ............................................................... VISUAL INSPECTION
WARNING
Even in the OFF position, an engine may fire. Always
treat a propeller as potentially dangerous. Do not take
position underneath a propeller at any time. Never
push/pull the propeller to move the aircraft.
Never move the propeller by hand.
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.11
FORWARD CABIN AIR INLETS ..................................................... CLEAR
NACELLE UNDERSIDE ............................................ VISUAL INSPECTION
Check for excessive contamination particularly by oil, fuel and
other fluids.
ANTENNAS ................................................................................ CHECK
GASCOLATOR ........................................................................... DRAIN
Check for water and sediment (drain until no water or sediment
comes out.
VENTING PIPES .......................................................................... CHECK
MISCELLANEOUS
With battery master switch ON, then OFF
FOR NIGHT FLIGHT ONLY:
INTERIOR LIGHTING .................................................... ON AND CHECK
EXTERIOR LIGHTING .................................................... ON AND CHECK
ALL LIGHTING SWITCHES ............................................................... OFF
FOR IMC FLIGHT ONLY:
PITOT HEAT ................................................................................... ON
PITOT HEAT ANNUNCIATOR .......................................... EXTINGUISHED
PITOT PROBE ................................................................. CHECK WARM
Care should be taken when an operational check of the heated pitot
head is performed. The unit becomes very hot. Ground operation
should be limited to 3 minutes to avoid damaging the heater ele-
ments.
WARNING
The exhaust can cause burns when hot.
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COCKPIT PREPARATION
REAR DOOR .......................................................... CLOSED & SECURED
RUDDER PEDALS ................................................. ADJUSTED & LOCKED
The rudder pedals may only be adjusted on the ground. The pedals
are unlocked by pulling the black handle which is located behind
the rear attachment. Forward adjustment: while keeping the handle
pulled, push the pedals forward with your feet to the desired posi-
tion. Release the handle and allow the pedals to lock in place. Rear-
ward adjustment: using the unlocking handle, pull the pedals back
to the desired position. Release the handle and allow the pedals to
lock in place.
The seating position should be the same for both VFR and IFR
flights. Most students tend to sit too high (wanting to see over the
nose of the aircraft) and too close to the instrument panel (making
scanning instruments more difficult). The instructor should advise
the student of the correct position. Verify that the pedals are locked
by applying pressure to try to move them.
FLIGHT CONTROLS ............................................... PROPER OPERATION
Check the flight controls for proper operation:
―Stick left, left aileron up, right aileron down, stick
right, right aileron up, left aileron down. Stick aft, elevator
up, stick forward, elevator down. Left rudder, right rudder‖.
Aileron and elevator deflections can be visually checked from the
pilot‘s seat.
SEATBELTS ............................................................................. LOCKED
Use of all available seat belts and/or harnesses per seat is manda-
tory. Seat belts of empty seats will be fastened and crossed over
the seat bottom to prevent control interference or passenger injury
during flight in turbulent air. Fasten belts before closing canopy.
Do not unlock seat belts during flight or taxi at any time.
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.13
AVIONICS MASTER SWITCH ........................................................... OFF
ELECTRIC MASTER SWITCH ............................................................. ON
Turn on both the BATT & ALT side. Allow the G1000 to initialize.
Check database validity on MFD. Press ‗ENT‘ twice on the MFD
(lower right softkey).
The G1000 will start its initialization process while the rest of the
cockpit preparation is done.
ESSENTIAL BUS SWITCH ................................................................. OFF
ALTERNATE STATIC VALVE ..................................................... CLOSED
INSTRUMENT PANEL
DIMMER CONTROL ......................................................................... SET
Use the rotary buttons to adjust instrument lighting and flood light.
Day flight: OFF. Night flight: as required (avoid setting the lights
too bright).
LIGHT SWITCHES ........................................................................... OFF
EMERGENCY SWITCH ...................................... CHECK OFF & GUARDED
STANDBY INSTRUMENTS ...................................................... CHECKED
MAGNETIC COMPASS ................................................................ CHECK
Check magnetic compass for normal reading, no bubbles in the
fluid and no leaks. Deviation chart present.
DEVIATION CARD ...................................................................... CHECK
ELT ........................................................................................... CHECK
Check red LED not flashing, if flashing press reset.
CIRCUIT BREAKERS ........................................................................... IN
CAUTION
With the ESS BUS ON, the battery will not be charged.
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If a circuit breaker needs resetting, check why it has tripped or
been pulled.
G1000 ........................................................................ ACKNOWLEDGE
Wait until power-up completed. Press ENT on MFD to acknowledge.
Note: the engine instruments are not available on the MFD until
acknowledged. Push the DISPLAY BACKUP button on the audio
panel to activate the G1000 reversionary (backup) mode. Push the
SYSTEM softkey on the MFD to activate the engine/system page.
FUEL QUANTITY ....................................................................... CHECK
FUEL CALCULATOR........................................................................ SET
TOTAL TIME IN SERVICE ............................................................. NOTE
Write down the G1000 total time in service.
G1000 ............................................................ BACKUP OR REV. MODE
IGNITION KEY ................................................................. READY & OFF
FUEL PUMP .................................................................................... OFF
PITOT HEAT .................................................................................. OFF
FLAPS .............................................................................................. UP
CENTER CONSOLE
ALTERNATE AIR ....................................................................... CLOSED
CABIN HEATER SWITCH ................................................................. OFF
DEFROSTER SWITCH ...................................................................... OFF
PARKING BRAKE ............................................................................ SET
The parking brake lever operates a one-way valve. Set the parking
brake, then pump the brake pedals with your feet to build up pres-
sure in the brake cylinders.
THROTTLE .................................................................................... IDLE
PROPELLER .......................................................................... HIGH RPM
MIXTURE .................................................................................... LEAN
FRICTION ............................................................................ ADJUSTED
FUEL TANK SELECTOR ................................................... LOWEST TANK
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.15
AVIONICS MASTER ......................................................................... ON
ATIS ............................................................................................ COPY
VFR OR IFR CLEARANCE .............................................................. COPY
Obtain from ATC or instructor.
AVIONICS MASTER ........................................................................ OFF
BRIEFING ............................................................................... PERFORM
Briefing must contain:
Pilot flying
Type of takeoff (normal or short field) and power/rpm.
Vr and Vclimb
Engine failure procedure
VFR and IFR departure procedure (routing)
Initial climb instructions+safety altitude (VFR or IFR) (altitude)
Crosscheck of the navaid setup (radios)
Example VFR:
―I fly normal takeoff, full power, 2700RPM, flaps take off, Vr
60, Vclimb 70. In case of engine failure, lower the nose, speed 75
clean, 70 with flaps, land straight ahead or slightly left or right. VFR
departure procedure: left closed traffic, 2200 feet‖.
Example IFR:
―I fly normal takeoff, full power, 2700RPM, flaps take off, Vr
60, Vclimb 70. In case of engine failure, lower the nose, speed 75
clean, 70 with flaps, land straight ahead or slightly left or right. IFR
departure procedure: left heading 190°, climb to 4000 feet‖.
Brief your passengers about seat belts (keep fastened during whole
flight), doors (how to open in an emergency), sick sacs (must ask for
them before it‘s too late!) and the intercom (explain that, in order to
respect the sterile cockpit concept during critical phases of flight, you
may isolate them from the crew).
―BEFORE START CHECKLIST‖
FRONT CANOPY ........................................................ POSITION 1 OR 2
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I N T E N T I O N A L L Y L E F T B L A N K
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.17
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ENGINE START
Starting with the external power source: perform procedure in read
-and do with DA40 AFM.
STROBE LIGHTS (DAY) OR POSITION LIGHTS (NIGHT) ...................... ON
ELECTRIC FUEL PUMP ..................................................................... ON
THROTTLE ................................................................. HALF WAY OPEN
MIXTURE ................................... RICH 5 SECONDS, THEN IDLE CUTOFF
THROTTLE .................................................................. 1/2 INCH OPEN
PROPELLER AREA ....................................................................... CLEAR
Check the area around the airplane. Open the window momentarily
and shout ―Prop clear‖.
IGNITION KEY ............................................................................ START
Turn the start key as required to start the engine, and release when
the engine has started. Do not overheat the starter motor. Do not
operate the starter motor for more than 10 seconds. After 1 start
cycle, apply a cooling period of 20 seconds. After 6 consecutive
start cycles, apply a cooling period of 30 minutes.
MIXTURE ........................................... FULL RICH (WHEN ENGINE FIRES)
THROTTLE .......................................................................... 1000 RPM
OIL PRESSURE ........................................................................... CHECK
If the oil pressure has not moved from the red range within 15
seconds after starting, shutdown the engine. Maintenance action is
due.
ELECTRIC FUEL PUMP .................................................................... OFF
WARNING
Do not start with the canopy open.
The canopy must be in position 1 or 2 to start.
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.19
ANNUNCIATIONS/ENGINE/SYSTEM PAGE ................................... CHECK
Check engine instruments on MFD from BOTTOM to TOP:
Fuel quantity: checked (keep running on lowest
tank until runup)
Volts: checked
AMPS: checked
Oil temperature: checked (will not yet indicate any-
thing since engine is cold)
CHT: checked (number inside triangle indicates
cylinder that is being measured)
Fuel pressure: checked
Fuel flow: checked
RPM: 1000 RPM
AVIONICS MASTER SWITCH ............................................................ ON
―AFTER START CHECKLIST‖
BEFORE TAXI
PITOT HEAT .............................................................................. CHECK
Switch pitot heat ON. Verify the amber PITOT HT OFF and STALL HT
OFF annunciations disappear from the PFD. Note an increase in AMP
output. Switch pitot heat OFF.
G1000 SETUP ...................................................................... COMPLETE
I—INITIALIZE PROFILE (AUX4—MAP—MFD FPL—PFD FPL)
F—FLIGHT PLAN
R—RADIOS (COMS—VOR—ADF—DME—CDI—BRG)
P—PERFORMANCE (SPEED BUGS)
Use the VFR and IFR (real or simulated) clearance (each item
chronologically) as a guideline to set radios and navaids. COM1:
ground frequency. COM1 will be the only radio used for ATC com-
munications during the whole flight. COM2 will be the radio dedi-
cated to ATIS and company communications during the whole
flight. NAV1: first VOR required by clearance, set first radial on HSI.
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NAV2: second VOR required by clearance, set radial on VOR indica-
tor. NAV1 and NAV2 will be used as follows: at all times VOR (or
LOC) in use on NAV1, next VOR on NAV2, DME and ADF: as re-
quired by clearance.
―BEFORE TAXI CHECKLIST‖
TAXI
Observe wing clearances when taxiing near buildings or other ob-
jects (buildings, poles, etc). Avoid holes and ruts when taxiing over
uneven ground. Do not operate the engine at high RPM when taxi-
ing over ground containing loose stones, gravel, any other loose
material, on a ramp or near a hangar to avoid damage to the pro-
peller blades and other nearby aircraft or objects.
TAXI LIGHT .................................................................................... ON
MIXTURE ..................................................................................... LEAN
Lean the mixture (approx. 1 inch).
The remedy is to run the engine at 2000 RPM for 2 minutes (oil and
cylinder head temperatures must remain in limits). Vapor lock can
be avoided if the engine is run at speeds of 1800 RPM or more.
This results in lower fuel temperature. Check the aircraft AFM
‗Chapter NORMAL OPERATING PROCEDURES—TAXIING‘ for more
information.
AREA ............................................................................................ FREE
Check the area around the airplane. Call out ―Left is free, free
right?‖ Instructor will reply ―Right is free‖. In case of solo flights, the
CAUTION
Following extended operation on ground (or at high ambient
temperatures) fuel vapor lock may occur, which will yield
following symptoms:
Random changes in IDLE RPM / FUEL FLOW
SLOW ENGINE RESPONSE
ENGINE WILL NOT RUN IN IDLE
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.21
call out will be ―Left is free, right is free‖ after having verified both
sides.
PARKING BRAKE ..................................................................... RELEASE
BRAKES ..................................................................................... CHECK
Perform brake check immediately after the aircraft starts rolling.
Apply light and even pressure on both pedals. It is not necessary to
bring the aircraft to a complete stop. As soon as it becomes appar-
ent that normal brake pressure is available, release the brakes
again. Ask the pilot in the right seat to perform a brake check as
follows ―Brakes checked, you have controls, check your
brakes‖. The right seat pilot will reply ―I have controls‖ and perform
the brake check, then he will announce ―Brakes, checked you have
controls‖. Pilot flying (left seat pilot) will reply ―I have controls‖ and
continue taxi.
Taxi turns can be made using rudder pedal motion only. Brakes are
only needed to reduce the taxi speed or when maneuvering in tight
spaces. On the ground and in flight, the pilot‘s feet should be in an
almost horizontal position-heels on the floor, toes on the lower
part of the rudder pedals-sliding the feet up on the rudder pedals
only when required to apply brakes.
FLIGHT INSTRUMENTS ............................................................... CHECK
In a left turn: "Turning left (=> check turn coordinator going
left), skidding right (=> check side slip going right), HSI and compass
decreasing (=> check numbers on HSI and magnetic compass
decreasing), horizon level (=> check attitude indicator level)".
In a right turn: "Turning right, skidding left, HSI and compass
increasing, horizon level".
The checks need to be done only once, in a left turn or a right turn,
outside congested area.
GROUND CHECK
NOSE WHEEL ........................................................................ STRAIGHT
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To prevent high side loads on the nose wheel. Wind more than 10
knots: turn the aircraft into the wind to avoid abnormal propeller
loads and to ensure adequate engine cooling during run-up. Wind
10 knots or less, park the aircraft in any convenient position where
prop wash cannot cause damage to an aircraft behind you. To pre-
vent a collision in case of inadvertent brake release during engine
run-up, never point the propellers in the direction of another air-
craft, and never ‗hook‘ your wing into the wing of another aircraft
parked ahead of you. When no run-up area available, perform the
ground check on the taxiway with the aircraft at an angle of ap-
proximately 30° referenced to the taxiway centerline.
PARKING BRAKE ............................................................................ SET
The parking brake lever operates a one-way valve. Set the parking
brake, then pump the brake pedals with your feet to build up pres-
sure in the brake cylinders.
ENGINE PAGE ........................................................................ NORMAL
Note that oil pressure may be in the yellow range with a warm en-
gine and throttle at IDLE.
MIXTURE ............................................................................. FULL RICH
FUEL TANK SELECTOR .................................................. FULLEST TANK
AREA BEHIND ............................................................................... FREE
Always check the area behind the aircraft before starting the
ground check, and call out: ―Area behind free‖.
THROTTLE .......................................................................... 2000 RPM
ALTERNATE AIR ..................................................... CHECK OPERATION
Observe +/- 25 RPM drop. CAUTION! Alternate air is unfiltered. Use
of alternate air during ground or flight operations when dust or
other contaminants are present may result in damage from particle
ingestion.
PROPELLER ................................................................................ CYCLE
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.23
Cycle the propeller 3 times. Do not allow the drop to exceed 300
RPM. First cycle: check RPM drop, second cycle, check MAP in-
crease, third cycle, check oil pressure decreasing.
MAGNETOS ............................................. CHECK (L—BOTH—R—BOTH)
Drop off on either magneto should not exceed 175 RPM and the
difference between the magnetos should not exceed 50 RPM.
Operation on 1 magneto should not exceed 10 seconds. If RPM
does not drop, flight is not permitted as a hot magneto exists
(faulty grounding of one side of the ignition system). If excessive
drop is noted, try to clear the spark plugs from lead deposits by
leaning the mixture (at 2000 RPM) to peak RPM, and then
rechecking the ignition. Company procedure: no full throttle runups
in the runup area allowed!
ENGINE PAGE ......................................................................... NORMAL
THROTTLE ......................................................... IDLE THEN 1000 RPM
Engine not faltering at idle RPM.
MIXTURE ..................................................................................... LEAN
Lean the mixture (approx. 1 inch).
BEFORE TAKEOFF
CONTROLS .................................................................................. FREE
CIRCUIT BREAKERS ........................................................................... IN
G1000 ............................................................................... REV. MODE
IGNITION ................................................................................... BOTH
FUEL PUMP..................................................................................... ON
FLAPS ............................................................................................. TO
Normal takeoff FLAPS UP (CRUISE), short field takeoff FLAPS T/O.
ALTERNATE AIR ...................................................................... CLOSED
PROPELLER ........................................................................... MAX RPM
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MIXTURE ....................................................................................... SET
TRIM ............................................................................................. SET
FUEL SELECTOR ............................................................ FULLEST TANK
SHORT BRIEFING .................................................................. PERFORM
The short briefing will include:
Type of takeoff (normal or short or soft)
Initial heading and altitude
―Confirmed?‖ The instructor answers ―Confirmed‖ or
amends as necessary.
Example VFR:
―Normal takeoff, heading 090°, 3.500FT, confirmed?‖ -
―Confirmed‖.
FRONT CANOPY ..................................................... CLOSED & LOCKED
DOOR WARNING................................................................ CHECK OFF
―BEFORE TAKEOFF CHECKLIST‖
LINE-UP
When ATC clearance (if required) received and acknowledged to line
up, FIRST release the parking brake and start to roll to the runway,
THEN perform the following actions (while taxiing). Fast taxi turns
immediately prior to takeoff should be avoided to prevent unport-
ing fuel feed lines. On request of PF ―Line-up items‖, the
starred * items may be performed by the PM.
APPROACH ................................................................................... FREE
Visually clear the final approach area before entering the runway
and call out: ―Approach free‖.
LANDING LIGHT ............................................................................. ON
TAXI LIGHTS .................................................................................. OFF
STROBE LIGHTS .............................................................................. ON
ALTIMETER ........................................................................ CHECK (3X)
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.25
Read threshold elevation from Jeppesen or other airport chart and
call out: ―Threshold elevation _____feet‖. This may be done
while taxiing out of the run-up area. Altimeter reading should not
differ more than 60 feet from threshold elevation at sea level and
80 feet at 5000 feet pressure altitude.
COMPASS SYSTEM .................................................. RUNWAY HEADING
This is a runway + compass system check. Read runway heading
from chart, takeoff data (QFU) and call out: ―Runway heading
_____ degrees‖. Check HSI and magnetic compass. Maximum differ-
ence allowed between published runway heading and any compass
system is 6°. If a large discrepancy exists, do not take off, but in-
vestigate the cause first (wrong runway, compass system malfunc-
tion).
PITOT HEAT .................................................................... AS REQUIRED
Switch pitot heat ON. Verify the amber PITOT HT OFF and STALL HT
OFF annunciations disappear from the PFD.
MIXTURE ......................................................................... AS REQUIRED
Set the mixture as required for takeoff.
TAKE-OFF
Before applying engine power for takeoff, top the timer and call
out: ―Takeoff, I have control‖. The instructor will confirm:
―You have control‖.
THROTTLE ............................................. GRADUALLY FULLY FORWARD
PARAMETERS ............................................................................ CHECK
Check:
ANNUNCIATIONS ...................................................................... CHECK
INSTRUMENTS ........................................................................... CHECK
MAP ............................................................................. STABILIZES 29‖
RPM ................................................................... STABILIZES 2700 RPM
Call out : ―Power checked‖.
QRH DA40-180
REV 1.3 —
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.26
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Note:
1. The proper performance of the engine at full throttle should
be checked early in the take-off procedure, so that the take-
off can be abandoned if necessary.
2. A rough engine, sluggish RPM increase, or failure to reach
take-off RPM (2680 +/- 20 RPM) are reasons for abandoning
take-off. If engine oil is cold, an oil pressure in the yellow
sector is permissible.
3. Takeoffs are made with full throttle.
Check airspeed increasing and call out: ―Speed checked‖.
At Vr, call out ―60 knots, rotate‖ and rotate smoothly to a BA
of 9°. Avoid abrupt, premature or late rotation. Climb 70 knots to
300 FT AGL, select flaps UP
AFTER TAKEOFF
As soon as the aircraft is in clean configuration 70 KIAS.: reduce
RPM by 300 => 2400 RPM. Keep full throttle. Above 1000 FT AGL
climb 75 knots, 2400RP (cruise climb)
Perform following actions at 1.000 FT AGL.
FLAPS .............................................................................................. UP
FUEL PUMP .................................................................................... OFF
Keep the fuel pump ON if remaining in the pattern.
ENGINE INSTRUMENTS .............................................................. CHECK
LANDING LIGHT ............................................................. AS REQUIRED
TRANSPONDER ................................................................. CODE & ALT
MAP PAGE ............................................................................... SWITCH
When out of the traffic pattern and congested area, switch off the
landing lights. Do not switch off the landing lights when remaining
in the traffic pattern , transiting controlled airspace or in the
practice area.
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.27
―AFTER TAKEOFF CHECKLIST‖
CLIMB
Enroute climb is 85 KIAS with 2400 RPM. Accelerate to this speed
when passing through 1.000 feet AGL for better forward speed,
engine cooling and increased visibility over the nose during climb.
CRUISE
Cruise checklist should be performed every 15 minutes.
FUEL STATUS ............................................................................ CHECK
Switching of tanks is required on a regular bases. Maximum allow-
able imbalance is 10 USG. When switching tanks, fuel pump should
be ON.
FUEL PUMP..................................................... ON AT HIGH ALTITUDES
ENGINE INDICATIONS / SYSTEM PAGE ....................................... CHECK
Mixture adjustment:
Best economy only allowed below 75% power (27 MAP / 2200
RPM or 26 MAP / 2400 RPM).
Use the G1000 leaning assistant.
Maximum CHT is 500°F.
Best economy: lean for peak EGT. Best power: lean 100°F rich
of peak EGT.
Enrichen each time for higher power settings (climb) or de-
scending to destination.
Cruise speed with 55% power (21 MAP / 2400 RPM) will be 120-125
KTAS (approx. 110 KIAS). Fuel flow will be approximately 8 GPH
(best economy).
DESCENT-APPROACH
When the altimeter setting for the destination airport is set:
QRH DA40-180
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.28
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LANDING LIGHT ............................................................................. ON
ALTIMETER ............................................................................. SET (3X)
Set local altimeter setting for the destination airport. Complete
answer to this checklist item is: ―_____(altimeter setting) set‖. Set
altimeter bug on pattern altitude when VFR, or on DA or MDA when
IFR.
ENGINE INDICATIONS / SYSTEM PAGE .................................. CHECKED
FUEL PUMP ..................................................................................... ON
MIXTURE ........................................................ ENRICHEN AS REQUIRED
FUEL SELECTOR .............................................................. AS REQUIRED
―DESCENT-APPROACH CHECKLIST‖
LANDING
Downwind:
FLAPS ............................................................................. AS REQUIRED
Turning base:
BRAKES ................................................................................ CHECKED
After checking the brakes, make sure to slide your feet back to the
normal position (heels on floor, toes on lower part of the pedals).
PARKING BRAKE ............................................................................ OFF
FLAPS ............................................................................. AS REQUIRED
PROPELLER ........................................................................... MAX RPM
MIXTURE ............................................................................. FULL RICH
―LANDING CHECKLIST‖
REV 1.3 —
QRH DA40-180
Document Level: 3
NORM PROC AIRLINE TRAINING CENTER, INC. 3.29
TOUCHDOWN
Maintain desired approach flight path with BA. Maintain desired
airspeed with power. Reduce power to idle during the flare before
the main wheels touch the runway. This gives the gear warning
horn a chance to blow if the gear is not locked down. After ground
contact, hold the nose wheel off as long as possible. Braking-if
needed–is most effective when back pressure is applied to the con-
trol wheel, putting most of the aircraft weight on the main wheels.
When the headwind component exceeds 15 knots, or when the
crosswind component exceeds 10 knots, as well as in gusty wind
conditions, the approach will be flown at a slightly higher than
normal speed (+5 KIAS) with T/O FLAPS.
AFTER LANDING
Runway vacated, aircraft stopped behind hold short line. On re-
quest of PF ―After landing items‖.
LANDING LIGHT ............................................................................ OFF
TAXI LIGHT .....................................................................................ON
TRANSPONDER ......................................................... CODE & GROUND
FUEL PUMP ................................................................................... OFF
PITOT HEAT .................................................................................. OFF
FLAPS ............................................................................................. UP
MIXTURE .................................................................................... LEAN
Lean the mixture (approx. 1 inch).
―AFTER LANDING CHECKLIST ―
SHUTDOWN
TAXI LIGHT ................................................................................... OFF
ENGINE/SYSTEM PAGE .......................................................... CHECKED
Write down the G1000 total time in service.
AVIONICS MASTER ........................................................................ OFF
MIXTURE ................................................................................ CUTOFF
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QRH DA40-180
REV 1.3 —
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STROBE LIGHTS ............................................................................. OFF
IGNITION KEY ...................................................... OFF & KEY REMOVED
ELECTRIC MASTER SWITCH ............................................................ OFF
PARKING BRAKE ............................................................. AS REQUIRED
Never taxi the aircraft facing fuel pumps with engines running, park
parallel to pumps. Stop with plenty of space, then pull the aircraft
forward into the fueling position. Do not set parking brake unless
on a slope.
―SHUTDOWN CHECKLIST‖
MOORING
PARKING BRAKE ..................................................................... RELEASE
Push aircraft backward or pull aircraft forward into parking space
using the tow bar for steering. Do not turn the nose gear beyond its
steering radius in either direction as this will result in damage to
the nose gear and steering mechanism.
TOW BAR ................................................................... STOW PROPERLY
SUNSCREENS, PITOT COVER, TIE-DOWN, CHOCKS .................. INSTALL
Tie-down ropes are required when the aircraft is left unattended
longer than for a normal crew change. If no tie-down ropes are
available on ramp, use the aircraft tie-down ropes (in flight gear
bag). Secure tie-down ropes to the wing tie-down rings and to the
tail skid at approximately 45° angles to the ground. Use bowline
knots, square knots or locked slip knots. Do not use plain slip
knots.
Parking brake is required when aircraft is not tied down, but with
the crew around. Do not set parking brake when the brakes are
overheated!
Wheel chocks are required when the aircraft is not tied down and
left unattended. If no wheel chocks available at the FBO, use the
aircraft‘s own wheel chocks (in flight gear bag).
NORM PROC AIRLINE TRAINING CENTER, INC. 3.30
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REV 1.3 —
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CONTROL LOCKS ................................................................... INSTALL
SEAT BELTS .................................................................................LOCK
Seat belts of all seats will be fastened.
PERSONAL BELONGINGS AND TRASH ...................................... REMOVE
CANOPY AND DOORS................................................ CLOSE & SECURE
Lock with key.
If required: fill in strip in aircraft squawk book and report problem
to dispatch and maintenance.
If required: fill in ASR.
Return aircraft key to dispatch.
If required: close flight plan.
NORM PROC AIRLINE TRAINING CENTER, INC. 3.31
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FLOWS ARE INTENDED TO PROVIDE A LOGICAL SEQUENCE IN WHICH THE ITEMS CAN BE DONE AND SHOULD BE FOLLOWED BY A CHECk-
LIST AT ALL TIMES, EXCEPT FOR THE WALKAROUND.
PRE—FLIGHT PREPARATION FLOW
ALL PERTINENT INFORMATION CONCERNING FLIGHT ................................... CHECK
FLIGHT RELEASE FORM .............................................................................COMPLETE
AIRPLANE SQUAWK BOOK ............................................................................. CHECK
EQUIPMENT REQUIRED FOR FLIGHT ............................................................... CHECK
AIRCRAFT KEYS AND POUCH ......................................................................... CHECK
I-M-S-A-F-E CHECKLIST .............................................................................. CHECK
MISSION BRIEFING ......................................................................................... CHECK
WALKAROUND FLOW
APPROACHING THE AIRCRAFT
NEARBY OBSTACLES ...................................................................................... CHECK
FLAP POSITION ................................................................................................ NOTE
SURFACES ...................................................................................................... CLEAR
ANTENNAS .................................................................................................... CHECK
PRELIMINARY INSPECTION
FRONT CANOPY & REAR DOOR ..................................................................... CHECK
FIRE EXTINGUISHER .................................................... CHECK SECURE / CONDITION
CONTROL LOCKS ........................................................................................ REMOVE
IGNITION KEY ............................................................... CHECK OFF & KEY REMOVED
HOBBS METER ............................................................................................... CHECK
UPPER SWITCH PANEL ................................................................. ALL SWITCHES OFF
LOWER SWITCH PANEL ................................................................ ALL SWITCHES OFF
PARKING BRAKE .................................................................................................. SET
ELECTRIC MASTER SWITCH.................................................................................. ON
FLAPS ................................................................................................. CHECK DOWN
FUEL GAUGES ............................................................................... CHECK QUANTITY
ELECTRIC MASTER SWITCH................................................................................. OFF
TRIM .......................................................................................................... NEUTRAL
SUNSCREENS, PITOT COVER, STALL WARNING COVER & TIE-DOWN ............. CHECK
CHOCKS ........................................................................................................ CHECK
TOWBAR ..................................................................................... PROPERLY STOWED
REQUIRED EQUIPMENT ............................................................................ ON BOARD
LEFT MAIN LANDING GEAR
LANDING GEAR STRUT .................................................................................. CHECK
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.33
WEAR, TREAD & DEPTH OF TIRE .................................................................... CHECK
WHEEL BRAKES / HYDRAULIC BRAKE LINE ...................................................... CHECK
SLIP MARKS.................................................................................................... CHECK
CHOCKS ......................................................................................................REMOVE
LEFT WING
WING SURFACE .............................................................................................. CHECK
STEP .............................................................................................................. CHECK
AIR INTAKES ON LOWER SURFACE ................................................................. CHECK
OPENINGS ON LOWER SURFACE ..................................................................... CHECK
TANK DRAIN .................................................................................................. CHECK
STALL WARNING DEVICE ................................................................................ CHECK
TANK FILLER .................................................................................... CHECK / CLOSE
STALL STRIPS ................................................................................................. CHECK
PITOT STATIC PROBE ..................................................................................... CHECK
TIE-DOWN ......................................................................................... CHECK/CLEAR
LANDING LIGHT / TAXI LIGHT ....................................................................... CHECK
WING TIP ....................................................................................................... CHECK
POSITION LIGHT / STROBE LIGHT .................................................................. CHECK
AILERON AND LINKAGE ................................................................................. CHECK
AILERON HINGES AND SAFETY PIN ................................................................. CHECK
FOREIGN OBJECTS IN AILERON PADDLE ......................................................... CHECK
FLAP AND LINKAGE ........................................................................................ CHECK
FLAP HINGES & SAFETY PIN ............................................................................ CHECK
FUSELAGE LEFT SIDE
CANOPY LEFT SIDE ........................................................................................ CHECK
REAR CABIN DOOR & WINDOW ........................................... CHECK / CLOSE & LOCK
FUSELAGE SKIN…………………………………………… ................. ………….…….CHECK
ANTENNAS.………………………………… .................................... ……………….CHECK
EMPANNAGE
STABILIZERS & CONTROL SURFACES/ELEVATOR TIPS..…… .................... ….…CHECK
HINGES……………………………………...…………………………… ................ .….CHECK
ELEVATOR TRIM TAB...……………….……….…………………… ................ ……..CHECK
RUDDER TRIM TAB………………......……………………………… ............... ...…..CHECK
TIE DOWN...……………………………………………… ............... ………...CHECK/CLEAR
TAIL SKID & LOWER FIN………...…………………………… ................ ……..……..CHECK
FUSELAGE RIGHT SIDE
QRH DA40-180
REV 1.3 —
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.34
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FUSELAGE SKIN…………………………………………… ................. ………….…….CHECK
WINDOW ............................................................................. CHECK / CLOSE & LOCK
CANOPY RIGHT SIDE ..................................................................................... CHECK
RIGHT WING
FLAP AND LINKAGE ....................................................................................... CHECK
FLAP HINGES & SAFETY PIN ........................................................................... CHECK
AILERON AND LINKAGE ................................................................................. CHECK
AILERON HINGES AND SAFETY PIN ................................................................ CHECK
FOREIGN OBJECTS IN AILERON PADDLE ......................................................... CHECK
WING TIP ....................................................................................................... CHECK
POSITION LIGHT / STROBE LIGHT.................................................................. CHECK
TIE-DOWN ......................................................................................... CHECK/CLEAR
WING SURFACE .............................................................................................. CHECK
STALL STRIPS ................................................................................................ CHECK
TANK FILLER .................................................................................... CHECK / CLOSE
OPENINGS ON LOWER SURFACE .................................................................... CHECK
TANK DRAIN ................................................................................................. CHECK
STEP .............................................................................................................. CHECK
RIGHT MAIN LANDING GEAR
LANDING GEAR STRUT .................................................................................. CHECK
WEAR, TREAD & DEPTH OF TIRE .................................................................... CHECK
WHEEL BRAKES / HYDRAULIC BRAKE LINE ..................................................... CHECK
SLIP MARKS ................................................................................................... CHECK
CHOCKS ...................................................................................................... REMOVE
FUSELAGE FRONT & NOSE GEAR
ENGINE OIL LEVEL ......................................................................................... CHECK
COWLING ...................................................................................................... CHECK
3 AIR INTAKES............................................................................................... CHECK
PROPELLER & SPINNER................................................................................... CHECK
NOSE LANDING GEAR STRUT ......................................................................... CHECK
WEAR, TREAD & DEPTH OF TIRE .................................................................... CHECK
SLIP MARKS ................................................................................................... CHECK
CHOCKS ...................................................................................................... REMOVE
EXHAUST ....................................................................................................... CHECK
FORWARD CABIN AIR INLETS ......................................................................... CHECK
NACELLE UNDERSIDE .................................................................................... CHECK
ANTENNAS .................................................................................................... CHECK
GASCOLATOR ................................................................................................ DRAIN
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.35
VENTING PIPES ............................................................................................... CHECK
MISCELLANEOUS
INTERIOR LIGHTING...……………………………… ................. ……………..ON & CHECK
EXTERIOR LIGHTING………………………………................... ………………ON & CHECK
ALL LIGHTING SWITCHES….…………………… .................. ……………………...…...OFF
PITOT HEAT..………………….………………… ................ ……………………………....ON
PITOT HEAT ANNUNCIATOR.………………… .................. ………………EXTINGUISHED
PITOT STATIC PROBE…………………………………… ..... ………………….CHECK WARM
PITOT HEAT……………………………………................... ……………………………….OFF
COCKPIT PREPARATION FLOW
REAR DOOR ............................................................................... CLOSED & SECURED
RUDDER PEDALS……………………………… .................. ….……..ADJUSTED & LOCKED
FLIGHT CONTROLS…………………………… .................. …...….…PROPER OPERATION
SEATBELTS.……………………………………… ................ .…….………………….LOCKED
AVIONICS MASTER SWITCH..…………...… ................. ……….………………………..OFF
ELECTRIC MASTER SWITCH.…………….. .................. ……….….……….……………...ON
ESSENTIAL BUS SWITCH..……………… ................... …..…….….……….…………….OFF
ALTERNATE STATIC VALVE ............................................................................ CHECK
DIMMER CONTROL……………………… ................ ...…………………………………...SET
LIGHT SWITCHES……………………… ................ ………………………………………..OFF
EMERGENCY SWITCH.…..…………… .................. ……………..CHECK OFF & GUARDED
STANDBY INSTRUMENTS……………… ................. ……………………………...CHECKED
MAGNETIC COMPASS..……………… ................. ….………………………………...CHECK
DEVIATION CARD..…………...………................ …..……………………………..CHECKED
ELT.……………………………………. ............ ………………………………………CHECKED
CIRCUIT BREAKERS..…… ................. …………….….……………….……..………………IN
G1000..………………… .............. ……………………..…………………...ACKNOWLEDGE
FUEL QUANTITY..……… .............. ……………………………………………...........CHECK
FUEL CALCULATOR.…… ................ ……………………………………………………….SET
TOTAL TIME IN SERVICE (HOBBS)………… ................. ..…………………………….NOTE
G1000……………………………………… ................ ……………..BACKUP OR REV MODE
IGNITION KEY ................................................................................. READY AND OFF
FUEL PUMP ..........................................................................................................OFF
PITOT HEAT ........................................................................................................OFF
FLAPS………………………………….…………… ................ ……………………………….UP
ALTERNATE AIR.………………………… ................. ………………………CHECK CLOSED
CABIN HEATER SWITCH.……………………………… ...... …….………………………….OFF
DEFROSTER SWITCH.………………………… .................. ………….……………………OFF
PARKING BRAKE.………………….…………… ................. ……………………………….SET
THROTTLE ......................................................................................................... IDLE
PROPELLER................................................................................................ HIGH RPM
QRH DA40-180
REV 1.3 —
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.36
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MIXTURE ...................................................................................................... CUTOFF
FRICTION LEVER ........................................................................................... ADJUST
FUEL SELECTOR.………………………………… .. ….…………………………LOWEST TANK
AVIONICS MASTER.……………….……………… .................…………………………….ON
ATIS/VFR OR IFR CLEARANCE.………………. ................. ……………………………COPY
AVIONICS MASTER.……………….……………… ............... …………………………….OFF
BRIEFING.……………….………………………… ................. ……………………..PERFORM
―BEFORE START CHECKLIST‖
FRONT CANOPY……..………………………… ................ ……….……..POSITION 1 OR 2
ENGINE START FLOW
STROBE LIGHTS (DAY) OR POSITION LIGHTS (NIGHT).………… .............. ………….ON
FUEL PUMP .......................................................................................................... ON
THROTTLE…………………………………………… .................. ……………….HALF OPEN
MIXTURE………………………….………………RICH FOR SECONDS THEN IDLE CUTOFF
THROTTLE…………………………………………… .. ……………….HALF 1/2 INCH OPEN
PROPELLER AREA………………………………………… ................... ….…………….CLEAR
IGNITION KEY……………………………………………… ............... ….……………..START
MIXTURE………………………….……………… ............. FULL RICH WHEN ENGINE FIRES
RPM………………………………………………….……… .................. ………………...1000
OIL PRESSURE ................................................................................................ CHECK
FUEL PUMP ......................................................................................................... OFF
ENGINE SYSTEM PAGE/VOLTAGE & AMPS…………… ................... ………………CHECK
AVIONICS MASTER SWITCH……………… ................. ……………………………………ON
―AFTER START CHECKLIST‖
BEFORE TAXI FLOW
PITOT HEAT……………………………… ................... ……………………………….CHECK
G1000 SET UP (I-F-R-P).…………………… ......... ………….…..…………..….COMPLETE
―BEFORE TAXI CHECKLIST‖
TAXI FLOW
TAXI LIGHT……………… ............... …………………………………………………………ON
MIXTURE………… ......................................................... ……………………………LEAN
AREA……………………… ................ ………….…..…………………………………..….FREE
PARKING BRAKE………… .................. …………………..…………………………..RELEASE
BRAKES…………………… ................ …………………………………………………..CHECK
FLIGHT INSTRUMENTS…… ................ ……………..………………………………...CHECK
REV 1.3 —
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.37
GROUND CHECK
NOSE WHEEL ............................................................................................. STRAIGHT
PARKING BRAKE .................................................................................................. SET
ENGINE PAGE .............................................................................................. NORMAL
MIXTURE………… .................................................. ……………………………FULL RICH
FUEL SELECTOR ................................................................................. FULLEST TANK
AREA BEHIND .................................................................................................... FREE
THROTTLE ................................................................................................ 2000 RPM
ALTERNATE AIR ..........................................................................CHECK OPERATION
PROPELLER......................................................................................................CYCLE
MAGNETOS .................................................................................................... CHECK
ENGINE PAGE .............................................................................................. NORMAL
THROTTLE ............................................................................. IDLE, THEN 1000 RPM
MIXTURE .......................................................................................................... LEAN
BEFORE TAKEOFF FLOW
CONTROLS..………………………………….……………… ................. ………………...FREE
CIRCUIT BREAKERS…………………………………… ................... ………………………..IN
G1000.……………………………………………… ................ …………………..REV. MODE
IGNITION ......................................................................................................... BOTH
FUEL PUMP ........................................................................................................... ON
FLAPS.……………………………………………….… ................................... ……………TO
ALTERNATE AIR ..................................................................................................OFF
PROPELLER................................................................................................. MAX RPM
MIXTURE .............................................................................................. AS REQUIRED
TRIM………………………………………………… ................. ………………….............SET
FUEL SELECTOR…………………………………… .. .…………………………FULLEST TANK
SHORT BRIEFING……………………………………................... .…………………PERFORM
FRONT CANOPY..………………………………….…… ................ …...CLOSED & LOCKED
DOOR WARNING…………………………………….… .................……………..CHECK OFF
―BEFORE TAKEOFF CHECKLIST‖
LINE UP FLOW
APPROACH..……………………………………….….................. ….…………………….FREE
LANDING LIGHTS ................................................................................................. ON
TAXI LIGHTS .......................................................................................................OFF
STROBE LIGHTS.................................................................................................... ON
ALTIMETER ............................................................................................. CHECK (3X)
COMPASS SYSTEM ......................................................................................... CHECK
PITOT HEAT ......................................................................................... AS REQUIRED
MIXTURE………… ............................................. ……………………………AS REQUIRED
QRH DA40-180
REV 1.3 —
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.38
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TAKEOFF FLOW
THROTTLE.................................................................. GRADUALLY FULLY FORWARD
PARAMETERS ................................................................................................. CHECK
AFTER TAKEOFF FLOW
FLAPS……………………………………………………… ................ …..…………………...UP
FUEL PUMP ......................................................................................................... OFF
ENGINE INSTRUMENTS…………………………… .................. ……………………...CHECK
LANDING LIGHT.……………………………..…… ............... ….………….....AS REQUIRED
TRANSPONDER…………………………………................ ………………….....CODE & ALT
MAP PAGE……………………………………… ................……..…………………….SWITCH
―AFTER TAKEOFF CHECKLIST‖
CRUISE FLOW
FUEL STATUS…………………………………………………………...… ………………CHECK
FUEL PUMP ......................................................................... USE AT HIGH ALTITUDES
ENGINE INDICATIONS / SYSTEM PAGE…………………………...… .... ……………CHECK
DESCENT / APPROACH FLOW
LANDING LIGHT……………………………… ............... …………………………………..ON
ALTIMETER..…………………………………… ............... ………….………………………ON
ENGINE INDICATIONS/SYSTEM PAGE…… .................. ….……………………..CHECKED
FUEL PUMP .......................................................................................................... ON
MIXTURE ............................................................................ ENRICHEN AS REQUIRED
FUEL SELECTOR………………………… .... …………………………………….AS REQUIRED
―DESCENT / APPROACH CHECKLIST‖
LANDING FLOW
BRAKES..……………………………………… ................. ……….………………….CHECKED
PARKING BRAKE…..………………………… ................ ……..……………………….....OFF
PROPELLER ................................................................................................ MAX RPM
MIXTURE .................................................................................................. FULL RICH
FLAPS………………………………………… ..................………….…...……..AS REQUIRED
―LANDING CHECKLIST‖
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.39
AFTER LANDING FLOW
LANDING LIGHT…… ................. ………………………………………..………………...OFF
TAXI LIGHT……………….................. ……………………………………..………………..ON
TRANSPONDER………… ................ ……………………………...….…..CODE & GROUND
FUEL PUMP ..........................................................................................................OFF
PITOT HEAT……………… ................ ………………………………….…………………..OFF
FLAPS……………………................. ……………………………….…….………………..…UP
MIXTURE .......................................................................................................... LEAN
―AFTER LANDING CHECKLIST‖
ENGINE SHUTDOWN FLOW
TAXI LIGHT…………………………… ............... ………………….……………………….OFF
ENGINE PAGE (TOTAL TIME IN SERVICE)…… .................. …....……………….CHECKED
AVIONICS MASTER………………………………… ................. ………..…………………OFF
MIXTURE …… .............................................................. ..….…………………..CUT OFF
STROBE LIGHTS (DAY) OR POSITION LIGHTS (NIGHT).………… ..............………….OFF
IGNITION KEY..……………………………………………… ................ ………………….OUT
ELECTRIC MASTER SWITCH…………………………….……. .................. ……………..OFF
PARKING BRAKE………………………………………… .................. …………AS REQUIRED
―SHUTDOWN CHECKLIST‖
MOORING FLOW
PARKING BRAKE.………… .................. ………………………………………………RELEASE
TOW BAR……………….………… .................. ……………….……………STOW PROPERLY
SUNSCREENS, STALL WARNING COVER, PITOT COVER…. ................... ……...INSTALL
CONTROL LOCKS ......................................................................................... INSTALL
SEAT BELTS………………………………………………….…… ................. …………...LOCK
PERSONAL ITEMS………………………………………….… ..................…….…….REMOVE
CANOPY………………………………………………... ............... ……....CLOSE AND LOCK
AIRCRAFT TIE DOWNS……………….……………… .................. .…………….....SECURED
QRH DA40-180
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.40
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BEFORE START CHECKLIST
WALK AROUND .............................................................................................. COMPLETED
RUDDER PEDALS ..................................................................... ADJUSTED AND LOCKED
SEAT BELTS ........................................................................................................... LOCKED
PARKING BRAKE ........................................................................................................... SET
AVIONICS MASTER SWITCH ........................................................................................ OFF
ELECTRIC MASTER SWITCH .......................................................................................... ON
ESSENTIAL BUS SWITCH ............................................................................................. OFF
CIRCUIT BREAKERS ......................................................................................................... IN
FLAPS ............................................................................................................ AS REQUIRED
G1000 ........................................................................................................ ACKNOWLEDGE
FUEL PUMP .................................................................................................................... OFF
FUEL QUANTITY.................................................................................................. CHECKED
IGNITION ............................................................................................... OFF & KEY READY
ALTERNATE AIR ..................................................................................................... CLOSED
THROTTLE ..................................................................................................................... IDLE
PROPELLER ......................................................................................................... MAX RPM
MIXTURE ................................................................................................................. CUTOFF
FUEL SELECTOR ........................................................................................ LOWEST TANK
AFTER START CHECKLIST
OIL PRESSURE ................................................................................................... CHECKED
ANNUNCIATORS/ENGINE/SYSTEM PAGE ....................................................... CHECKED
BEFORE TAXI CHECKLIST
PITOT HEAT ......................................................................................................... CHECKED
G1000 SET UP ................................................................................................ COMPLETED
BEFORE TAKEOFF CHECKLIST
FLIGHT INSTRUMENTS ...................................................................................... CHECKED
ENGINE INSTRUMENTS ..................................................................................... CHECKED
FLAPS ............................................................................................................................... T/O
FUEL PUMP ...................................................................................................................... ON
IGNITION ...................................................................................................................... BOTH
MIXTURE ....................................................................................................... AS REQUIRED
PROPELLER ......................................................................................................... MAX RPM
FUEL SELECTOR ....................................................................................... FULLEST TANK
TRIM ................................................................................................................................ SET
FLIGHT CONTROLS .................................................................................................... FREE
CANOPY & DOORS .......................................................................... CLOSED & SECURED
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NORM PROC AIRLINE TRAINING CENTER, INC. 3.41
AFTER TAKEOFF CHECKLIST
These items only when remaining in the pattern
FLAPS ...................................................................................................................... UP
FUEL PUMP .................................................................................................................... OFF
ENGINE INSTRUMENTS ................................................................................. CHECK
LANDING LIGHT ........................................................................................... AS REQUIRED
DESCENT APPROACH CHECKLIST
These items only when remaining in the pattern
LANDING LIGHTS ............................................................................................................ ON
ALTIMETER .............................................................................................................SET (2X)
ENGINE INDICATIONS/SYSTEM PAGE .................................................... CHECKED
FUEL PUMP ...................................................................................................................... ON
FUEL SELECTOR .............................................................................. FULLEST TANK
LANDING CHECKLIST
BRAKES ..................................................................................................................... CHECK
PARKING BRAKE ........................................................................................................... OFF
PROPELLER ..........................................................................................................MAX RPM
MIXTURE ............................................................................................................. FULL RICH
FLAPS ........................................................................................................... AS REQUIRED
AFTER LANDING CHECKLIST
LANDING LIGHT ............................................................................................................. OFF
TAXI LIGHT ....................................................................................................................... ON
TRANSPONDER ..................................................................................... CODE & GROUND
FUEL PUMP .................................................................................................................... OFF
PITOT HEAT ................................................................................................................... OFF
FLAPS ............................................................................................................................... UP
MIXTURE ...................................................................................................................... LEAN
SHUTDOWN CHECKLIST
AVIONIC MASTER SWITCH .......................................................................................... OFF
MIXTURE ................................................................................................................. CUTOFF
IGNITION KEY ............................................................................................... OFF AND OUT
ELECTRIC MASTER SWITCH ....................................................................................... OFF
PARKING BRAKE ......................................................................................... AS REQUIRED
PILOT OVERHEAD READING LIGHT ............................................................. CHECK OFF
I N T E N T I O N A L L Y L E F T B L A N K
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EMER
PROC
I N T E N T I O N A L L Y L E F T B L A N K
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.1
G1000 WARNINGSG1000 WARNINGSG1000 WARNINGS
Warning Page Description
OIL PRES LO 4.4 Oil pressure low (red range)
FUEL PRES LO 4.5 Fuel pressure low (red range)
FUEL PRES HI 4.5 Fuel pressure high (red range)
(No procedure)
ALTERNATOR 4.5 Alternator failure
STARTER ENGD 4.6 Starter not disengaging
DOOR OPEN 4.6 Unlocked doors
OTHER EMERGENCY PROCEDURESOTHER EMERGENCY PROCEDURESOTHER EMERGENCY PROCEDURES
Situation Page Situation Page
EMERGENCY LANDING 4.3 TOTAL ELECTRICAL
FAILURE 4.9
WINDMILL
ENGINE RESTART 4.3 ENGINE FIRE
4.9
4.10
SPIN RECOVERY 4.6 ELECTRICAL FIRE 4.10
4.11
ENGINE ROUGHNESS /
POWER LOSS 4.7
SUSPICION CARBON
MONOXIDE 4.11
RPM OVERSPEED 4.7 UNINTENTIONAL FLIGHT IN
ICING 4.11
RPM UNDERSPEED 4.8 LDG WITH DEFECTIVE
BRAKES 4.12
POWERED
ENGINE RESTART 4.8
LDG WITH DEFECTIVE
MAIN TIRE 4.12
QRH DA40-180
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.2
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G1000 CAUTIONS
Warning Page Description
PITOT OFF 4.13 Pitot heating system OFF
PITOT FAIL 4.13 Pitot heating system failed
L FUEL LOW Left tank fuel qty low (<3 USG)
R FUEL LOW Right tank fuel qty low (<3 USG)
VOLTS LOW 4.13 Bus voltage too low
OTHER ABNORMAL PROCEDURES
Situation Page Situation Page
OIL TEMP HIGH 4.14 FUEL FLOW HIGH 4.15
CHT HIGH/ LOW 4.15 VOLTS HIGH 4.16
EGT HIGH/ LOW 4.15 MAP HIGH 4.16
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.3
EMERGENCY LANDINGEMERGENCY LANDINGEMERGENCY LANDING
1 AIRSPEED .. 75KIAS, 70 FLAPS T/O or 60 FLAPS LDG 2 TRANSPONDER .............................. SQUAWK 7700 3 MAYDAY CALL ....................................... PERFORM 4 FUEL SELECTOR ............................................. OFF 5 MIXTURE ........................................ IDLE CUT-OFF 6 IGNITION ....................................................... OFF 7 FLAPS .............................................. AS REQUIRED When flaps extension not required anymore 8 MASTER SWITCH ............................................ OFF 9 SEAT BELTS & HARNESSES ....................... TIGHTEN
WINDMILL ENGINE RESTARTWINDMILL ENGINE RESTARTWINDMILL ENGINE RESTART
(ENGINE FAILURE)(ENGINE FAILURE)(ENGINE FAILURE)
1 AIRSPEED ............................................ 75-80 KIAS 2 FUEL SELECTOR ............................. FULLEST TANK 3 IGNITION .................................................... BOTH 4 MIXTURE ..............................................FULL RICH 5 FUEL PUMP ..................................................... ON 6 ALTERNATE AIR ........................................... OPEN If no success 7 MIXTURE .................... LEAN then SLOWLY to RICH
If no success, Perform EMERGENCY LANDING Checklist
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.4
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1 OIL PRESS ................................................. CHECK 2 OIL TEMP .................................................. CHECK 3 CYL HEAD TEMP ........................................ CHECK If Oil Temp & Cyl Head Temp are normal. 4 OIL TEMP & CYL HEAD TEMP ................. MONITOR Land at Nearest suitable airport If Oil Temp & Cyl Head Temp are NOT normal ( or ris-ing). 5 ENGINE POWER ............................ REDUCE TO MIN Land ASAP, be prepared for Emergency Landing. If Oil Press near zero, vibration, loss of oil, smoke. 6 TOTAL ENGINE FAILURE .......................... SUSPECT 7 ENGINE............................................. SHUT DOWN Perform the Emergency Landing Checklist
OIL PRES LOOIL PRES LOOIL PRES LO
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.5
1 FUEL FLOW ................................................ CHECK If Fuel Flow high (red range), suspect fuel leak. Land ASAP
1 CIRCUIT BREAKERS .................................... CHECK 2 ALTERNATOR LOAD ................................... CHECK 3 MASTER SWITCH (ALT) ..................... OFF, then ON If warning disappears and Alternator Load is normal Continue normal operations If warning remains 4 ESSENTIAL BUS ................................................ON 5 ELECTRICAL LOAD ................................... REDUCE Land within 30 minutes If PFD attitude information is lost 6 HORIZON EMERGENCY SWITCH ........................ON
1 FUEL FLOW ................................................ CHECK Land at nearest suitable airfield
FUEL PRES LO
FUEL PRES HI
ALTERNATOR
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.6
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1 THROTTLE .................................................... IDLE 2 MIXTURE ......................................... IDLE CUT OFF 3 IGNITION ....................................................... OFF 4 MASTER SWITCH ............................................. OFF Do NOT attempt restart.
1 AIRSPEED ................................................. REDUCE 2 CANOPY AND REAR DOOR .......... CHECK VISUALLY 3 CANOPY / REAR DOOR ...............................LATCH If unable to latch door Land ASAP Warning! Never unlatch rear door in flight.
STARTER ENGD
DOOR OPEN
SPIN RECOVERYSPIN RECOVERYSPIN RECOVERY
Perform items 1-4 immediately & simultaneously. 1 THROTTLE .................................................... IDLE 2 RUDDER ................. FULL IN OPPOSITE DIRECTION 3 ELEVATOR .................................... FULL FORWARD 4 AILERONS............................................... NEUTRAL 5 FLAPS ..............................................................UP When rotation stops 6 RUDDER ................................................. NEUTRAL 7 ELEVATOR .................................. PULL CAREFULLY Regain level flight, but do NOT exceed Vne
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.7
ROUGH ENGINE / POWER LOSSROUGH ENGINE / POWER LOSSROUGH ENGINE / POWER LOSS
1 AIRSPEED ................................................. 75 KIAS 2 FUEL PUMP ......................................................ON 3 FUEL SELECTOR ................................... CHECK ON 4 ENGINE INSTRUMENTS ............................... CHECK 5 THROTTLE & PROPELLER ............................ CHECK 6 MIXTURE .................... SET FOR SMOOTH RUNNING 7 ALTERNATE AIR ........................................... OPEN
If no success or insufficient power 10 EMERGENCY LANDING ........................... PERFORM
Perform EMERGENCY LANDING Checklist as appropriate.
RPM OVERSPEEDRPM OVERSPEEDRPM OVERSPEED
1 FRICTION ................................................. ADJUST 2 OIL PRESSURE ............................................ CHECK
If Oil Pressure is low, adjust RPM with Throttle. Perform OIL PRES LO Checklist
If Oil Pressure is normal, adjust RPM with Propeller control or with Throttle.
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.8
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RPM UNDERSPEEDRPM UNDERSPEEDRPM UNDERSPEED
1 FUEL PUMP ...................................................... ON 2 FUEL SELECTOR ......................................... CHECK 3 FRICTION ..................................................ADJUST 4 PROPELLER ........................................... HIGH RPM If no success, adjust RPM with Throttle Land ASAP
POWERED ENGINE RESTARTPOWERED ENGINE RESTARTPOWERED ENGINE RESTART
Warning: Only perform this checklist if the propeller is NOT windmilling and NO damage to the engine. 1 AIRSPEED ................................................. 80 KIAS 2 ELECTRICAL LOAD.................................... REDUCE 3 AVIONICS MASTER SWITCH ............................. OFF 4 MASTER SWITCH ............................................. ON 5 MIXTURE ........................................................ SET 6 FUEL SELECTOR .............................. FULLEST TANK 7 FUEL PUMP ...................................................... ON 8 ALTERNATE AIR ........................................... OPEN 9 IGNITION ................................................... START
Note:
By increasing the airspeed above approximately 130 KIAS, the propeller will begin to rotate and the engine can thus be started. For this the ignition switch should be set to both. Refer to WINDMILLING ENGINE RESTART Checklist. An altitude loss of at least 1000‘ (300m) must be allowed for.
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.9
TOTAL ELECTRICAL FAILURETOTAL ELECTRICAL FAILURETOTAL ELECTRICAL FAILURE
1 CIRCUIT BREAKERS ....................... CHECK & RESET Note: reset CB only once 2 ESSENTIAL BUS ................................................ON If PFD information is lost. 3 HORIZON EMER SWITCH ...................................ON 4 FLOOD LIGHT .................................. AS REQUIRED 5 FLAPS......................................... CHECK POSITION Fly the airplane using Attitude & Power lever / Engine noise settings. Land ASAP
ENGINE FIREENGINE FIREENGINE FIRE
IN FLIGHT: Emergency landing is imminent! 1 CABIN HEAT .................................................. OFF 2 FUEL SELECTOR ............................................. OFF 3 THROTTLE .................................................... FULL 4 FUEL PUMP .................................................... OFF 5 EMER WINDOW / CANOPYOPEN IF NECESSARY
To control smoke in cockpit. Perform the EMERGENCY LANDING Checklist as appro-priate.
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.10
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ENGINE FIREENGINE FIREENGINE FIRE
ON GROUND: 1 AIRCRAFT .................................................... STOP 2 FUEL SELECTOR .............................................. OFF 3 CABIN HEAT ................................................... OFF
When aircraft is Stopped
4 THROTTLE ................................................... FULL 5 MASTER SWITCH (BAT) .................................... OFF 6 IGNITION ....................................................... OFF 7 CANOPY & REAR DOOR ................................ OPEN Evacuate airplane
ELECTRIC FIRE / SMOKEELECTRIC FIRE / SMOKEELECTRIC FIRE / SMOKE
IN FLIGHT: 1 HORIZON EMER SWITCH .................................. ON 2 EMER WINDOW / CANOPY ...... OPEN AS NECESSARY
To control smoke in cockpit.
3 ALT + BAT MASTER SWITCHES ........................ OFF 4 CABIN HEAT ................................................... OFF If Electronics / Avionics are required 5 (BAT) MASTER SWITCH ................................... ON 6 ESSENTIAL BUS ................................................ ON If smoke decreases Land ASAP If smoke persists 7 (ALT) MASTER SWITCH .................................... ON 8 ESSENTIAL BUS ............................................... OFF 9 BATT and ESS TIE CB‘s ...................................PULL Land ASAP
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.11
ELECTRICAL FIRE / SMOKEELECTRICAL FIRE / SMOKEELECTRICAL FIRE / SMOKE
ON GROUND: 1 BAT MASTER SWITCH ..................................... OFF 2 THROTTLE..................................................... IDLE 3 MIXTURE ......................................... IDLE CUT OFF When engine and aircraft stopped. 4 CANOPY ...................................................... OPEN Evacuate aircraft
SUSPICION CARBON MONOXIDESUSPICION CARBON MONOXIDESUSPICION CARBON MONOXIDE
1 CABIN HEAT .................................................. OFF 2 VENTILATION .............................................. OPEN 3 EMERGENCY WINDOW .................................. OPEN 4 CANOPY ............................................... UNLATCH
UNINTENTIONAL FLIGHT IN ICINGUNINTENTIONAL FLIGHT IN ICINGUNINTENTIONAL FLIGHT IN ICING
1 PITOT HEAT ....................................................ON 2 CABIN HEAT ....................................................ON 3 DEFROSTER .....................................................ON 4 PROPELLER .................................... INCREASE RPM 5 ALTERNATE AIR ........................................... OPEN 6 EMERGENCY WINDOW ............. OPEN AS REQUIRED Leave Icing area If Pitot Heat fails 7 ALTERNATE STATIC AIR ............................... OPEN 8 EMERGENCY WINDOW ................................. CLOSE
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LANDING WITH DEFECTIVE BRAKESLANDING WITH DEFECTIVE BRAKESLANDING WITH DEFECTIVE BRAKES
Plan to land on the LONGEST runway available, make a normal landing. After landing (if required) 1 FUEL SELECTOR .............................................. OFF 2 MIXTURE ......................................... IDLE CUT OFF 3 IGNITION ....................................................... OFF 4 MASTER SWITCH ............................................ OFF Avoid obstacles with rudder steering. Stop on the runway, do NOT attempt to taxi.
LANDING WITH DEFECTIVE MAIN TIRELANDING WITH DEFECTIVE MAIN TIRELANDING WITH DEFECTIVE MAIN TIRE
Plan to land on the WIDEST runway available, make a normal landing. Advise ATC. Make a normal landing except:
Land on the Rwy side of the good tire Keep wing on good side low Use rudder and brakes to maintain directional con-trol.
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1 PITOT HEAT ........................................ CHECK ON If in icing conditions. Expect Pitot-Static system failure, erratic instrument indications. 2 ALTERNATE STATIC AIR ............................... OPEN 3 ICING AREA ................................................ LEAVE
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.13
ON GROUND: 1 RPM ................................ INCREASE TO 1200 RPM 2 ELECTRICAL LOAD ................................... REDUCE 3 AMMETER & VOLTMETER ............................ CHECK If light still on, terminate flight.
IN FLIGHT: 1 ELECTRICAL LOAD ................................... REDUCE 2 AMMETER & VOLTMETER ............................ CHECK If light still on Perform ALTERNATOR FAIL Checklist
PITOT FAIL
VOLTS LOW
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OIL PRESSURE HIGH
1 OIL TEMP .................................................. CHECK If Oil temp is normal Land at nearest suitable airport If Oil temp is not normal Land ASAP
OIL TEMPERATURE HIGH
1 CHT & EGT ............................................... CHECK If CHT & EGT are normal. LANSA If EGT or CHT high. 2 OIL PRESSURE............................................ CHECK If Oil Press is low. >> Go to OIL PRES LO Emergency checklist item 5 Land ASAP If Oil Press is normal 3 MIXTURE .................................................. ENRICH 4 POWER .................................................... REDUCE If no success Land ASAP
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EMER PROC AIRLINE TRAINING CENTER, INC. 4.15
1 MIXTURE ...................................................... ENRICH 2 OIL TEMPERATURE ......................................... CHECK If Oil Temp is high. >>Go to OIL TEMPERATURE HIGH Checklist item 2
CYLINDER HEAD TEMP (CHT) or EGT HIGH
A very low reading for a single cylinder may be the re-sult of a loose sensor. Continue normal operations.
CYLINDER HEAD TEMP (CHT) or EGT LOW
1 FUEL PRES LO WARNING ................................... CHECK If on, suspect Fuel leak. Land ASAP If NOT on, continue normal operations. Use fuel flow figures from AFM. 2 FUEL QTY ...................................... CHECK REGULARLY
FUEL FLOW HIGH
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OVER VOLTAGE
1 ESSENTIAL BUS ..................................................... ON 2 ALT MASTER SWITCH ........................................... OFF 3 BAT MASTER SWITCH ........................................... ON 4 ELECTRICAL LOAD......................................... REDUCE Land at nearest suitable airfield
MANIFOLD PRESSURE HIGH
If clearly above green range, suspect faulty reading.
EMER PROC AIRLINE TRAINING CENTER, INC. 4.16
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PATTERNS
I N T E N T I O N A L L Y L E F T B L A N K
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PATTERNS AIRLINE TRAINING CENTER, INC. 5.1
NORMAL
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FLAPLESS
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PATTERNS AIRLINE TRAINING CENTER, INC. 5.3
POWER OFF
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POWER OFF FROM
DOWNWIND
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PATTERNS AIRLINE TRAINING CENTER, INC. 5.5
PRECAUTIONARY
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PREC APP
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PATTERNS AIRLINE TRAINING CENTER, INC. 5.7
NON PREC APP
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CIRCLING
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LIMITATIONS
I N T E N T I O N A L L Y L E F T B L A N K
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LIMITATIONS AIRLINE TRAINING CENTER, INC. 6.1
AIRSPEED LIMITATIONS
Speed Definition Limitation Indicator Marking
Never Exceed Speed
(Vne) 178 KIAS Red radial line
Maximum Structural
Cruising Speed (Vno) 129 KIAS End of green arc
Design Maneuvering
Above 2.161 lbs up to
2.535 lbs
Below 2.161 lbs
108 KIAS
94 KIAS
Maximum Flaps
Extended Speed
Takeoff (T/O)
Landing (LDG)
108 KIAS
91 KIAS
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LIMITATIONS AIRLINE TRAINING CENTER, INC. 6.2
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POWERPLANT LIMITATIONS
Definition Limitation Indicator Marking
Rotational Speed
Max Takeoff
Max Continuous
2700 RPM
2400 RPM
Red line
CHT MAX 500°F
Oil Temperature MAX 245°F Red line
Oil Quantity MIN 4 QTS
MAX 8 QTS
Oil Pressure MIN 25 PSI
MAX 98 PSI Red line
Fuel Grade 100 LL
Fuel Pressure MIN 14 PSI
MAX 35 PSI Red line
WEIGHT LIMITATIONS
Max Takeoff Weight
Normal Category
Utility Category
2.535 lbs
2.161 lbs
Max Landing Weight 2.535 lbs
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LIMITATIONS AIRLINE TRAINING CENTER, INC. 6.3
WEIGHT LIMITATIONS
Max Weights in Baggage
Compartments
Standard Baggage Compartment 66 lbs
Tube 11 lbs
MANEUVER LIMITS
NORMAL CATEGORY
All intentional acrobatic maneuvers (including spinning) and normal flight
maneuvers with more than 60° bank are prohibited.
UTILITY CATEGORY
All intentional acrobatic maneuvers (including spinning) and normal flight
maneuvers with more than 90° bank are prohibited.
FLIGHT MANEUVERING LOAD FACTORS
At VA At VNE With FLAPS
NORMAL
CATEGORY +3.8 / -1.52 +3.8 / 0 +2.0
NORMAL
CATEGORY +4.4 / -1.76 +4.4 / -1 +2.0
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LIMITATIONS AIRLINE TRAINING CENTER, INC. 6.4
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FUEL LIMITATIONS
Total Fuel Capacity 2 x 20.6 = 41.2 USG
Unusable Fuel 2 x 0.5 = 1 USG
Usable Fuel 40.2 USG
Max Indicated Fuel Tank Quantity
(per tank) 15 USG
Max Permissible Unbalance
(between L and R Tank) 10 USG
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6.5
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LIMITATIONS AIRLINE TRAINING CENTER, INC.
TEMPERATURE LIMITATIONS
Flight operations will be discontinued once temperature
reaches 43°C.
If a flight is arriving back to home base and ATIS reports 43°C
only a full stop landing will be made.
No touch and go operations with temperatures above 43°C.
COMPANY LIMITATIONS
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6.6 LIMITATIONS
AIRLINE TRAINING CENTER, INC.
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AIRCRAFT LEANING PROCEDURES
At density altitudes of 5000ft or above the aircraft should be
leaned for takeoff with the following procedure after the run-
up is completed.
-Full power
-Lean mixture slowly till EGT reaches 1350°-1400°
-Reduce power to 1000 RPM
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WEIGHT &
BALANCE
I N T E N T I O N A L L Y L E F T B L A N K
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WEIGHT & BALANCE AIRLINE TRAINING CENTER, INC. 7.1
ITEM ARM (IN) WEIGHT (LBS) MOMENT (IN-LBS)
BEW
PILOT & FRONT
PASSENGER 90.6
AFT PASSENGERS 128.0
BAG COMP (MAX 66 LBS) 143.7
BAG TUBE
(MAX 11 LBS) 170.1
ZFW
FUEL IN TKS
(40 USG MAX) 103.5
RW
FUEL ALLOWANCE
(START-TAXI) 103.5 -6 -621
TOW
(MAX 2535 LBS)
TRIP FUEL 103.5
LW
(MAX 2535 LBS)
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AIRCRAFT WEIGHT (LBS) MOMENT (IN-LBS)
N4106G 1722.0 166506.77
N4139B 1718.0 165990.08
N4189U 1719.0 165960.43
N4191M 1722.0 165840.79
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PERFORMANCE AIRLINE TRAINING CENTER, INC. 8.1
TAKEOFF DISTANCE—50FT UP TO 1,150 KG (2,535 LBS) .. 8.2
CRUISING TAS ................................................................ 8.3
LANDING DISTANCE ....................................................... 8.4
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PERFORMANCE AIRLINE TRAINING CENTER, INC. 8.2
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TAKEOFF DISTANCE
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PERFORMANCE AIRLINE TRAINING CENTER, INC. 8.3
CRUISING TAS
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PERFORMANCE AIRLINE TRAINING CENTER, INC. 8.4
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LANDING DISTANCE
Full Throttle Flight Training
AIRLINE TRAINING CENTER, INC.
CAE Global Academy, Phoenix
Sabena Airline Training Center
5010 East Falcon Drive, Suite 201
Mesa, AZ 85215
Phone +1 480 948 4515
Fax +1 480 443 88 61
satc@sabena-az.com
Sabena Flight Academy N.V.
Brussels National Airport Building 201
1820 Steenokkerzeel
Belgium
Phone +32 (0)2 75 25 711
Fax +32 (0)2 75 25 741
info@sfa.be
www.sfa.be
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